Aircraft Rinse System

Abstract

Disclosed is an aircraft rinse system for gently rinsing an aircraft engine even while the aircraft engines are on. The rinse deck has integral nozzles and water storage. Pressurized air can be used to force the water from the storage area in the deck to spray out nozzles that are integral to the deck.

Description

[0001]This is a continuation-in-part of application Ser. No. 11 / 004,321 filed on Dec. 12, 2004, which is a continuation-in-part of application Ser. No. 10 / 820,538 filed Apr. 8, 2004, now U.S. Pat. No. 7,291,267, which claims the benefit of U.S. Provisional Application No. 60 / 540,492, filed Jan. 30, 2004, the disclosures of which are incorporated herein by reference.STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT[0002]Not applicable.NAMES OF THE PARTIES TO A JOINT RESEARCH AGREEMENT[0003]Not applicable.INCORPORATION BY REFERENCE OF MATERIAL SUBMITTED ON A COMPACT DISC[0004]Not applicable.BACKGROUND OF THE INVENTION[0005]1. Technical Field[0006]The present invention relates to methods and apparatus for the physical separation of solids from fluids, and fluids from gases and the incorporation of same in a novel aircraft rinse system. More specifically, the invention relates to methods and apparatus for separating solids and dissolved constituents from fluids using an ar...

AI Technical Summary

Benefits of technology

[0021]These embodiments of the invention provide an economic and environmentally sound system for rinsing aircraft of different types and allow that such rinsing can take place without the aircraft shutting down its engine(s). Consequently, helicopters, for example, can be easily rinsed every day at the end of the last flight and prior to engine shutdown. Such capability greatly reduces the amount of corrosion that such aircraft experience by removing corrosive elements from the aircraft on a frequent basis, thereby reducing aircraft downtime and maintenance expenses.

Problems solved by technology

The safe and effective removal of contaminants from fluids is a consistent problem faced by many industries.

The presence of suspended and / or dissolved solids in water, wastewater and other fluids is undesirable for several reasons.

If established discharge-contamination levels are exceeded, cities and other governmental authorities may impose surcharges and penalties on the entity responsible for the excessive discharge.

Detergents and other chemicals used in the wash operations and drilling operations present further difficulties only increasing the effluent fluid discharge concerns.

However, where the cost of water is not a factor and the public sewage system can accept certain contaminants, a complete recycling system may not be cost justified.

Aircraft are particularly susceptible to corrosion, particularly when flown in highly-corrosive environments, such as near salt water and in areas with dust and blowing sand.

Aircraft that operate in these corrosive environments require frequent and expensive maintenance as a result of corrosion.

This not only adds to the cost of maintenance of these aircraft, but also increases the down time and unavailability of the aircraft.

Unfortunately, many airports and military facilities where aircraft rinses would occur are located remotely from water treatment facilities and lack drainage systems for collecting, storing, and treating the used rinse fluid.

Since the used rinse fluid may contain contaminants, it is undesirable that the fluid be allowed to contaminate the surrounding area or be deposited in a standard sewage system.

Previous attempts to address these issues have not been altogether successful.

The process described by the '758 patent is relatively expensive and would require frequent maintenance to keep the various filters serviceable.

The '758 patent also does not disclose an effective rinse system that can be used by various size aircraft, including helicopters, prior to final engine shutdown.

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